Heat Flux and Pressure Envelope Expansion Tests of Phenolic Impregnated Carbon Ablator (PICA)
Flight Test of a Resistive Heating Coating for Visualizing Flow Transition
Dynamic Finite Element Model Correlation
A Stratospheric Test Methodology for Characterizing Free-Flight Dynamics of Entry Vehicles
Accurate Simulation of Flows with Convected Vortices: Cartesian TAU
Simulation of Maximum Lift Using URANS for a High-Lift Transport Configuration
Improved Transition and Reynolds Stress Modeling in RANS Simulations
Nonlinear Reduced Order Modeling for Aeroelastic Simulation with Neural Networks
Response Surface Methods for Efficient Aerodynamic Surrogate Models
Transonic Tail Buffet Simulations on the ATRA Research Aircraft
Projection-Based Model Order Reduction for Steady Aerodynamics
Variable-Fidelity and Reduced-Order Models for Aero Data for Loads Predictions
Coupling Strategies for Large Industrial Models
Guidance and Control Techniques for Titan Aerogravity Assist for Enceladus Observation
Near Earth Asteroid Scout Spacecraft Design and Test
Rocket Plume-Surface Interaction Simulations for Moon and Mars Landings
Quiet VTOL Projects - NIFS Exit Presentation
PRANDTL-M: Designing a New Mars Gilder
Design for Minimum Casualty Area – The IXPE Case
Spectral Characterization of Modern Spacecraft Materials
Overview of the Acoustic Testing of the European Service Module Structural Test Article (E-STA)
Modeling of Movable Control Surfaces and Atmospheric Effects
Industrial ComFliTe Applications
NASTRAN Based Static CFD-CSM Coupling in FlowSimulator
Goniometric and Polarized Imaging Spectroscopic Lab Measurements of Spacecraft Materials
Small Satellite-sized Hypersonic Inflatable Decelerators (HIAD) for Interplanetary Science Missions
Flight Envelope Assessment of SmallSat Aerocapture Trajectories at Venus and Mars
NASA's Human Landing System: Enabling the next generation of lunar science
DLR Pilot Applications in ComFliTe
Industrialization of the Automatic Transition Prediction in the DLR TAU Code
Supersonic Transport Optimization to Mach 4
Commissioning the James Webb Space Telescope
DARPA - NASA Demonstration Rocket for Agile Cislunar Operation (DRACO)
Preliminary Results of UAS Quadcopter Aeroacoustics Testing
Comparison and Validation of Vortex Lattice Aerodynamic Analysis for the Learjet 24
Multi-component Modeling with the Dual Mesh Connect Approach
AMG in TAU: Adjoint Equations and Mesh Deformation
Mode Projection Method for Target Mode Identification
Enhancement of Damage Detectability in Aircraft Structures Using the Fusion of NDT Results
Spacecraft Materials Degradation Under Space-Simulated Low Earth Orbit (LEO) Environment
Spacecraft Materials Degradation Under Space-Simulated Low Earth Orbit (LEO) Environment